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You searched for: subject:"subsonic"
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[image]SWG Side window - NASA/Langley Research Center
Wide Body Subsonic Transport Side Window Panel
Keywords: Subsonic Transport
Downloads: 4
[image]SWG Side window - NASA/Langley Research Center
Wide Body Subsonic Transport Side Window Panel
Keywords: Subsonic Transport
Downloads: 4
[image]SWG Side window - NASA/Langley Research Center
Wide Body Subsonic Transport Side Window Panel
Keywords: Subsonic Transport
Downloads: 5
[image]SWG Side window - NASA/Langley Research Center
Wide Body Subsonic Transport Side Window Panel
Keywords: Subsonic Transport
Downloads: 11
[image]SWG Side window - NASA/Langley Research Center
Wide Body Subsonic Transport Side Window Panel
Keywords: Subsonic Transport
Downloads: 4
[audio]IUMA: Subsonic USA
Formed in 2000. Based in Nashville. Simply straight-up rock. Not even their own members can really put a finger on their style. It's a complex mix of heavy thundering metal, classic rock riffs, punkish attitudes, heartfelt lyrics, catchy melodies, and whatever else they can think of to throw on the fire! Their music takes you up into elation, back down into fury, and everywhere in between and to the edge of excitement - like a fun-filled rollercoaster without a guard rail! Opened for Jackyl and ...
Keywords: Subsonic USA
Downloads: 45
[image]SWG Side window - NASA/Langley Research Center
Wide Body Subsonic Transport Side Window Panel
Keywords: Subsonic Transport
Downloads: 4
[texts]Summary of the lift, drag, and stability of 1/10-scale rocket-boosted models of the mc donnell xf3h-1 airplane for a mach number range of 0.6 to 1.4 as affected by the operation of extensible rocket racks - Crabill, N. L.
No Abstract Available
Keywords: DRAG; STABILITY; SUBSONIC SPEED
Downloads: 90
[unknown]Wiki - subsonic
subsonic dumped with WikiTeam tools.
Keywords: wiki; wikiteam; MediaWiki; subsonic; sourceforgenet_apps_mediawiki_subsonic; unknowncopyright
[image]Pathfinder I controls wind model B - NASA/Langley Research Center
Photographed on 07/22/96. -- 1) +10 degrees outboard aileron B, 2) -10 degrees outboard aileron B, 3) right wing with temperature sensitive paint 4) general shot of Pathfinder I controls wing model B - subsonic transport model. In building 1236, shop area.
Keywords: SCALE MODELS -- SUBSONIC AIRCRAFT -- WIN
Downloads: 2
[image]Pathfinder I controls wind model B - NASA/Langley Research Center
Photographed on 07/22/96. -- 1) +10 degrees outboard aileron B, 2) -10 degrees outboard aileron B, 3) right wing with temperature sensitive paint 4) general shot of Pathfinder I controls wing model B - subsonic transport model. In building 1236, shop area.
Keywords: SCALE MODELS -- SUBSONIC AIRCRAFT -- WIN
Downloads: 3
[image]Elliptical wing model - NASA/Langley Research Center
Photographed on: 07/14/2000 and 07/17/2000. -- Elliptical wing model in the 14 x 22 Foot Subsonic Tunnel.
Keywords: WIND TUNNEL MODELS. -- SUBSONIC WIND TUN
Downloads: 4
[image]Elliptical wing model - NASA/Langley Research Center
Photographed on: 07/14/2000 and 07/17/2000. -- Elliptical wing model in the 14 x 22 Foot Subsonic Tunnel.
Keywords: WIND TUNNEL MODELS. -- SUBSONIC WIND TUN
Downloads: 6
[image]Elliptical wing model - NASA/Langley Research Center
Photographed on: 07/14/2000 and 07/17/2000. -- Elliptical wing model in the 14 x 22 Foot Subsonic Tunnel.
Keywords: WIND TUNNEL MODELS. -- SUBSONIC WIND TUN
Downloads: 3
[image]Elliptical wing model - NASA/Langley Research Center
Photographed on: 07/14/2000 and 07/17/2000. -- Elliptical wing model in the 14 x 22 Foot Subsonic Tunnel.
Keywords: WIND TUNNEL MODELS. -- SUBSONIC WIND TUN
Downloads: 10
[image]Elliptical wing model - NASA/Langley Research Center
Photographed on: 07/14/2000 and 07/17/2000. -- Elliptical wing model in the 14 x 22 Foot Subsonic Tunnel.
Keywords: WIND TUNNEL MODELS. -- SUBSONIC WIND TUN
Downloads: 2
[image]Elliptical wing model - NASA/Langley Research Center
Photographed on: 07/14/2000 and 07/17/2000. -- Elliptical wing model in the 14 x 22 Foot Subsonic Tunnel.
Keywords: WIND TUNNEL MODELS. -- SUBSONIC WIND TUN
Downloads: 6
[image]Elliptical wing model - NASA/Langley Research Center
Photographed on: 07/14/2000 and 07/17/2000. -- Elliptical wing model in the 14 x 22 Foot Subsonic Tunnel.
Keywords: WIND TUNNEL MODELS. -- SUBSONIC WIND TUN
Downloads: 2
[texts]Rocket-powered-model investigation of the effects of aeroelasticity on the rolling effectiveness of an 8.06-percent-scale mcdonnell f3h-1 airplane wing at mach numbers from 0.5 to 1.4 - English, R. D
No Abstract Available
Keywords: AEROELASTICITY; MACH NUMBER; SUBSONIC SPEED; WINGS
Downloads: 86
[texts]Drag and static stability at low lift of rocket-powered models of the convair mx-1626 airplane at mach numbers from 0.7 to 1.5 - Hall, J. R.
No Abstract Available
Keywords: DRAG; STATIC STABILITY; SUBSONIC SPEED; YAW
Downloads: 92
[texts]Some effects of aeroelasticity on the rolling effectiveness of a 10-percent-scale model of the mc donnell f-101a airplane wing at mach numbers from 0.5 to 1.2 - English, R. D
No Abstract Available
Keywords: AEROELASTICITY; MACH NUMBER; SUBSONIC SPEED; WINGS
Downloads: 89
[image]Elliptical wing model - NASA/Langley Research Center
Photographed on: 07/14/2000 and 07/17/2000. -- Elliptical wing model in the 14 x 22 Foot Subsonic Tunnel.
Keywords: WIND TUNNEL MODELS. -- SUBSONIC WIND TUN
Downloads: 2
[image]Elliptical wing model - NASA/Langley Research Center
Photographed on: 07/14/2000 and 07/17/2000. -- Elliptical wing model in the 14 x 22 Foot Subsonic Tunnel.
Keywords: WIND TUNNEL MODELS. -- SUBSONIC WIND TUN
Downloads: 6
[image]Elliptical wing model - NASA/Langley Research Center
Photographed on: 07/14/2000 and 07/17/2000. -- Elliptical wing model in the 14 x 22 Foot Subsonic Tunnel.
Keywords: WIND TUNNEL MODELS. -- SUBSONIC WIND TUN
Downloads: 7
[texts]INVESTIGATION OF THE ROLLING STABILITY DERIVATIVES OF TWO HYPERSONIC GLIDERS OF PARABOLIC PLAN FORM AT HIGH SUBSONIC SPEEDS - Arabian, D. D
Rolling stability derivatives of hypersonic gliders at subsonic speeds
Keywords: HYPERSONIC GLIDERS; ROLL; STABILITY DERIVATIVES; SUBSONIC SPEED; YAW; HYPERSONIC GLIDER; ROLL; STABILITY DERIVATIVE; SUBSONIC SPEED
Downloads: 93
[texts]SUMMARY OF SUBSONIC-DIFFUSER DATA - Henry, J. R.
Subsonic-diffuser data - exit flow, boundary-layer control, and inlet velocity
Keywords: BOUNDARY LAYER CONTROL; DIFFUSERS; SUBSONIC SPEED; WOOD; BOUNDARY LAYER CONTROL; DIFFUSER; EXIT; INLET; SUBSONIC SPEED
Downloads: 278
[texts]High mach number, low-cowl-drag, external- compression inlet with subsonic dump diffuser - Connors, J. F.
Low cowl drag, external compression inlet with subsonic dump diffuser for high Mach number application
Keywords: AIR INTAKES; SUBSONIC FLOW; ANNULI; DIFFUSERS; DRAG; MACH NUMBER; SUBSONIC FLOW; AIR INLET; DIFFUSER; INLET
Downloads: 109
[texts]Investigation of three low-temperature-ratio combustor configurations in a 48-inch-diameter ram-jet engine - Meyer, C. L.
No Abstract Available
Keywords: ANALOG SIMULATION; BLUNT BODIES; SUBSONIC SPEED; DYNAMIC STABILITY; STATIC STABILITY
Downloads: 74
[texts]A CDMA Spotbeam Architecture for the Next Generation Satellite System (NGSS) for the Aeronautical Telecommunications Network (ATN) - Raghavan, Rajesh S.
This paper will present work being done to model and simulate a CDMA based Mobile Satellite System architecture for providing all or part of the future Air Traffic Management (ATM) services. Such a system, will help in relieving the dependence on ground based networks, if not eliminate it. Additionally such an architecture can be used in parallel or as a supplementary service along with ground based links to help alleviate any capacity bottlenecks, or in areas where such services are difficult t...
Keywords: SUBSONIC SPEED; COMPRESSIBLE FLOW; MATHEMATICAL MODELS; DOWNWASH; FLOW VELOCITY
Downloads: 103
[movies]Erinyes - OresteS
All the music of OresteS is free to share http://www.dogmazic.net/orestes Licence C reaction in english http://morne.free.fr/Necktar7/creaction.htm
Keywords: colibri necrophile; horsnorme; clip; subsonic; experimental; industrial; drone; noise; orestes
Downloads: 39
[texts]SOME CONSTRUCTION PRINCIPLES FOR REMOTE CONTROL IMITATIVE MANIPULATORS - BOR-RAMENSKIY, A. Y.
SOME BASIC MECHANICAL REQUIREMENTS FOR THE CONSTRUCTION OF MANIPULATORS DESIGNED TO PERFORM A WIDE RANGE OF COMPLEX TASKS AT A DISTANCE FROM THE OPERATOR ARE REVIEWED. THE KINEMATICS AND DYNAMICS OF THE HUMAN ARM AND HAND ARE OUTLINED, AND RELEVANT CONSTRUCTION PRINCIPLES ARE ABSTRACTED. THESE PRINCIPLES ARE THEN, RATHER EFFECTIVELY, APPLIED TO IMITATIVE REMOTE CONTROL MANIPULATORS WITH BOTH ACTION AND PASSIVE FEEDBACK.
Keywords: CURVATURE; DIFFUSERS; SLOTS; AXISYMMETRIC FLOW; SUBSONIC FLOW; SUCTION
Downloads: 138
[audio]Amygdaloides - Asaguare
Soft and low ambience with infrasonic backbone.Part 14 in the 'Cranial Acres' series, a compilation of psychedelic and experimental sound installations.
Keywords: minimal; ambient; instrumental; downtempo; experimental; postmodern; psychedelic; subsonic; synth; chill
Downloads: 87
[texts]Calculation of a jet axis in a drifting flow - Shandorov, G. S
Deflection calculated for jet subject to drift in uniform unbounded subsonic gas flow
Keywords: DEFLECTION; SUBSONIC FLOW; FLOW DEFLECTION; GAS FLOW; JET FLOW; SUBSONIC FLOW; UNIFORM FLOW; FLOW DEFLECTION; GAS FLOW; JET FLOW
Downloads: 105
[texts]The calculation of flow in a plane Laval nozzle - Alikhashkin, Ya. I.
Uniform gas flow calculation for subsonic and transonic part of plane symmetrical Laval nozzle
Keywords: CONVERGENT-DIVERGENT NOZZLES; GAS FLOW; SUBSONIC SPEED; TRANSONIC FLOW; UNIFORM FLOW; DE LAVAL NOZZLE; GAS FLOW; SUBSONIC SPEED; TRANSONIC FLOW
Downloads: 168
[texts]THRUST AND PUMPING CHARACTERISTICS OF A SERIES OF EJECTORTYPE EXHAUST NOZZLES AT SUBSONIC AND SUPERSONIC FLIGHT SPEEDS - Hearth, D. P.
Thrust and pumping characteristics of ejector-type exhaust nozzles at subsonic and supersonic speeds
Keywords: EJECTORS; SUPERSONIC NOZZLES; SUPERSONIC SPEED; EJECTOR; EXHAUST NOZZLE; NOZZLE; PUMPING; SUBSONIC WIND TUNNEL; SUPERSONIC NOZZLE; EXHAUST NOZZLES; FREE FLOW; HEARTHS; PUMPING; SHROUDS; SUBSONIC SPEED; SUBSONIC WIND TUNNELS; SUPERSONIC FLIGHT
Downloads: 110
[texts]SOME EFFECTS OF VARIATIONS IN DENSITY AND AERODYNAMIC PARAMETERS ON THE CALCULATED FLUTTER CHARACTERISTICS OF FINITE-SPAN SWEPT AND UNSWEPT WINGS AT SUBSONIC AND SUPERSONIC SPEEDS - Yates, E. C., Jr
Subsonic and supersonic flutter calculations on swept and unswept wings to evaluate effects of variations in aerodynamic parameters and density
Keywords: AERODYNAMIC CHARACTERISTICS; UNSWEPT WINGS; AERODYNAMIC CHARACTERISTICS; FLOW CHARACTERISTICS; GAS DENSITY; SUBSONIC FLUTTER; SUPERSONIC FLUTTER; UNSWEPT WING; FLOW CHARACTERISTICS; FLUTTER ANALYSIS; GAS DENSITY; SUBSONIC FLUTTER; SUBSONIC SPEED; SUPERSONIC FLUTTER; SUPERSONIC SPEED; SWEPT WINGS
Downloads: 126
[texts]Effects of wing-fuselage flow fields on missile loads at subsonic speeds - Alford, W. J., Jr
Swept wing-fuselage flow fields on missile loads at subsonic speeds
Keywords: BODY-WING CONFIGURATIONS; SUBSONIC SPEED; SWEPT WING; WING-FUSELAGE COMBINATION; FLOW DISTRIBUTION; FUSELAGES; LOADS (FORCES); MISSILES; SUBSONIC SPEED; SWEPT WINGS; FLOW FIELD; MISSILE
Downloads: 87
[texts]DYNAMIC MODEL TESTS AT LOW SUBSONIC SPEEDS OF PROJECT MERCURY CAPSULE CONFIGURATIONS WITH AND WITHOUT DROGUE PARACHUTES - Bowman, J. S., Jr
Mercury capsule at subsonic speed with and without drogue parachute - dynamic model tests
Keywords: DRAG CHUTES; MERCURY CAPSULE; SUBSONIC SPEED; DYNAMIC MODELS; MERCURY PROJECT; MERCURY SPACECRAFT; SPACE CAPSULES; SPACECRAFT; SUBSONIC SPEED; TOWED BODIES; DROGUE PARACHUTE
Downloads: 89
[texts]Radiation Control with Selectively Reflective Overcoats - White, Susan M
Selectively reflective overcoats can be used to significantly reduce the temperature of a heated surface under conditions where short-wavelength radiation is the predominant mode of heat transfer to the surface and the total heating is below the melting or ablation limit. In addition, these overcoats can he used to detect and characterize radiation. Theoretical models are used to predict the optical properties of selectively reflective overcoats on an opaque substrate, such as metal or reaction-...
Keywords: AERODYNAMIC CHARACTERISTICS; LANDING SPEED; MACH NUMBER; STABILITY; SPACECRAFT CONFIGURATIONS; SUBSONIC SPEED; SUPERSONIC SPEED; HYPERSONICS; SINGLE STAGE TO ORBIT VEHICLES; LONGITUDINAL STABILITY; CONTROLLABILITY; SUBSONIC FLOW
Downloads: 59
[texts]LIQUID HYDROGEN AS A JET FUEL FOR HIGH-ALTITUDE AIRCRAFT - Hall, E. W.
Liquid hydrogen as jet fuel for high-altitude aircraft
Keywords: COMPARISON; LIQUID HYDROGEN; SUBSONIC AIRCRAFT; SUPERSONIC AIRCRAFT; HIGH ALTITUDE; JET ENGINE FUELS; JP-4 JET FUEL; LIQUID HYDROGEN; SUBSONIC AIRCRAFT; SUPERSONIC AIRCRAFT; HIGH ALTITUDE; JET FUEL
Downloads: 246
[texts]Factors affecting lateral stability and controllability - Campbell, J. P.
No Abstract Available
Keywords: AERODYNAMIC DRAG; PRESSURE DISTRIBUTION; SUBSONIC FLOW; THIN WINGS; LIFT; SUBSONIC WIND TUNNELS; SWEPT WINGS; WIND TUNNEL TESTS; AERODYNAMIC COEFFICIENTS; AIRCRAFT MODELS; HIGH ASPECT RATIO; MACH NUMBER
Downloads: 108
[texts]EXPERIMENTAL INVESTIGATION OF A HIGH SUBSONIC MACH NUMBER TURBINE HAVING HIGH ROTOR BLADE SUCTION-SURFACE DIFFUSION - Hauser, C. H.
Investigation of high subsonic turbine with high rotor blade suction-surface diffusion
Keywords: DIFFUSION; SUBSONIC SPEED; SURFACE DIFFUSION EFFECT; TURBINE BLADE; MACH NUMBER; ROTOR BLADES; SUBSONIC SPEED; SUCTION; SURFACE DIFFUSION; TURBINE BLADES; TURBINES; ROTOR BLADE
Downloads: 118
[texts]Stability and control characteristics at low subsonic speeds of an airplane configuration having two types of variable-sweep wings - Spencer, B., Jr
Static stability and control at low subsonic speeds of supersonic aircraft with variable sweep wings
Keywords: STABILITY; SWEPT WING; VARIABLE SWEEP; STATIC STABILITY; SUBSONIC SPEED; SUPERSONIC AIRCRAFT; SWEPT WINGS; VARIABLE SWEEP WINGS; STATIC STABILITY AND CONTROL; SUBSONIC SPEED; SUPERSONIC AIRCRAFT
Downloads: 135
[texts]THE SUBSONIC AERODYNAMIC CHARACTERISTICS OF SOME BLUNT DELTA CONFIGURATIONS WITH 75 DEG SWEEPBACK - Edwards, G. G.
Aerodynamic characteristics of blunt delta configurations with 75 deg sweepback and varying thickness distributions at subsonic speeds
Keywords: AERODYNAMIC CHARACTERISTICS; YAW; AERODYNAMIC CHARACTERISTICS; BLUNT BODY; DELTA WING; SUBSONIC SPEED; SWEEPBACK; ANGLE OF ATTACK; BLUNT BODIES; DELTA WINGS; FUSELAGES; SIDESLIP; SUBSONIC SPEED; SWEEPBACK; THICKNESS
Downloads: 127
[texts]NASTRAN structural model for the large 64-meter antenna pedestal. Part 2: Improved model - Chian, C. T
Static analysis and a computer structural model for the large 64-m antenna pedestal are developed using the MSC version of the NASTRAN program. This improved pedestal model includes the launch areas and the actual pressure pattern of the oil under the hydrostatic bearing pad. The results obtained from the new improved model have indicated that the deflections due to pad loads are in good agreement with field measurements...
Keywords: DELTA WINGS; FUSELAGES; VORTEX FLAPS; FLOW CHARACTERISTICS; LONGITUDINAL STABILITY; SUBSONIC FLOW; TRAILING EDGE FLAPS
Downloads: 29
[texts]Magnetic storm effects on cosmic rays in the solar activity minimum - Dorman, L. I., et al
No Abstract Available
Keywords: AIRCRAFT MODELS; SIDESLIP; STATIC STABILITY; SUBSONIC SPEED; FINS; LATERAL STABILITY; LONGITUDINAL STABILITY; VENTRAL SECTIONS
Downloads: 87
[texts]Mars spacecraft on a super long journey - Vesnyankin, L
A popularly written sketch of the various Mars probes of different countries is presented.
Keywords: AERODYNAMIC DRAG; JET EXHAUST; JET FLOW; LIFT AUGMENTATION; PITCHING MOMENTS; SWEPT WINGS; NOZZLE FLOW; SUBSONIC SPEED
Downloads: 89
[texts]On the question of efficient extraction of electrons from a plasma in a vacuum - Kreyndel, Yu. YE., et al
Efficient electron extraction from plasmas in vacuum
Keywords: AERODYNAMIC COEFFICIENTS; TABS (CONTROL SURFACES); UNSTEADY FLOW; MATHEMATICAL MODELS; MATRICES (MATHEMATICS); SUBSONIC FLOW; TWO DIMENSIONAL FLOW
Downloads: 76
[texts]Technical problems of commercial flying - Warner, Edward
The technical requirements for commercial aircraft are listed, which include: safety, economy and comfort. The author lists various methods to increase these requirements in commercial aircraft.
Keywords: FLOW - BODIES, ROTATING; COMPRESSIBLE; FLOW - CYLINDERS, CIRCULAR; FLOW VELOCITY, HIGH - SUBSONIC; THEORIES - FLOW; LINEAR
Downloads: 61
[texts]Measurements of pressure drop with no heat addition on mockup segments of the General Electric air-cooled aircraft reactor - Nagey, T. F.
No Abstract Available
Keywords: AERODYNAMIC CHARACTERISTICS; SUBSONIC FLOW; X-20 AIRCRAFT; AIRCRAFT CONFIGURATIONS; WIND TUNNEL MODELS
Downloads: 89
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